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EN 2282:1992
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Aerospace series - Characteristics of aircraft electrical supplies
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SAE AIR 6464 : 2013
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EUROCAE/SAE WG80/AE-7AFC HYDROGEN FUEL CELLS AIRCRAFT FUEL CELL SAFETY GUIDELINES
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RTCA DO 347 : 2013
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CERTIFICATION TEST GUIDANCE FOR SMALL AND MEDIUM SIZED RECHARGEABLE LITHIUM BATTERIES AND BATTERY SYSTEMS
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RTCA DO 178 : C2011
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SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
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ISO 11119-2:2012
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Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 2: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450 l with load-sharing metal liners
|
|
MIL-STD-704 Revision F:2004
|
AIRCRAFT ELECTRIC POWER CHARACTERISTICS
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SAE AIR 825/13 : 2003
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GUIDE FOR EVALUATING COMBUSTION HAZARDS IN AIRCRAFT OXYGEN SYSTEMS
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SAE AIR 1957 : 2015
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HEAT SINKS FOR AIRBORNE VEHICLES
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SAE ARP 4418 : 2008
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PROCEDURE FOR SAMPLING AND MEASUREMENT OF ENGINE AND APU GENERATED CONTAMINANTS IN BLEED AIR SUPPLIES FROM AIRCRAFT ENGINES
|
|
SAE ARP 4754 : 2010
|
GUIDELINES FOR DEVELOPMENT OF CIVIL AIRCRAFT AND SYSTEMS
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|
SAE AS 8010 : 2012
|
AVIATOR'S BREATHING OXYGEN PURITY STANDARD
|
|
MIL-DTL-7891 Revision G:2008
|
FILLER VALVE, AIRCRAFT OXYGEN
|
|
RTCA DO 254 : 2000
|
DESIGN ASSURANCE GUIDANCE FOR AIRBORNE ELECTRONIC HARDWARE
|
|
RTCA DO 227 : A2017
|
MINIMUM OPERATIONAL PERFORMANCE STANDARDS (MOPS) FOR NON-RECHARGEABLE LITHIUM BATTERIES
|
|
IEC 60952-3:2013
|
Aircraft batteries - Part 3: Product specification and declaration of design and performance (DDP)
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SAE J 2601 : 2016
|
FUELING PROTOCOLS FOR LIGHT DUTY GASEOUS HYDROGEN SURFACE VEHICLES
|
|
IEC 60952-2:2013
|
Aircraft batteries - Part 2: Design and construction requirements
|
|
SAE ARP 4761 : 1996
|
GUIDELINES AND METHODS FOR CONDUCTION THE SAFETY ASSESSMENT PROCESS ON CIVIL AIRBORNE SYSTEMS AND EQUIPMENT
|
|
SAE ARP 5021 : 2016
|
OXYGEN CYLINDER INSTALLATION GUIDE
|
|
RTCA DO 293 : A2009
|
MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR NICKEL-CADMIUM, NICKEL METAL-HYDRIDE, AND LEAD ACID BATTERIES
|
|
SAE ARP1870A:1987(S2012)
|
Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and Safety(STABILIZED Aug 2012)<br>
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|
SAE AS 861 : 2016
|
MINIMUM GENERAL STANDARDS FOR OXYGEN SYSTEMS
|
|
SAE AIR 1277 : 2005
|
COOLING OF MILITARY AVIONIC EQUIPMENT
|
|
SAE ARP 1532 : 2015
|
AIRCRAFT OXYGEN SYSTEM LINES, FABRICATION, TEST AND INSTALLATION
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|
SAE AIR 1059 : 2014
|
OXYGEN CYLINDER QUALITY, SERVICEABILITY, MAINTENANCE TRANSFILLING AND MARKING
|
|
EN 2570 : 1996
|
AEROSPACE SERIES - NICKEL-CADMIUM BATTERIES - TECHNICAL SPECIFICATION
|
|
FAA AC 20-184 : 2015
|
GUIDANCE ON TESTING AND INSTALLATION OF RECHARGEABLE LITHIUM BATTERY AND BATTERY SYSTEMS ON AIRCRAFT
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|
SAE J 2579 : 2013
|
STANDARD FOR FUEL SYSTEMS IN FUEL CELL AND OTHER HYDROGEN VEHICLES
|
|
SAE AIR 1168/8 : 2011
|
AIRCRAFT FUEL WEIGHT PENALTY DUE TO AIR CONDITIONING
|
|
ISO 11119-1:2012
|
Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 1: Hoop wrapped fibre reinforced composite gas cylinders and tubes up to 450 l
|
|
FAA AC 25.1309-1 : 0
|
SYSTEM DESIGN AND ANALYSIS
|
|
SAE AIR 64 : 1992
|
ELECTRICAL AND ELECTRONIC EQUIPMENT COOLING IN COMMERCIAL TRANSPORTS
|
|
IEC 60952-1:2013
|
Aircraft batteries - Part 1: General test requirements and performance levels
|
|
AIAA G 095 : 2004
|
GUIDE TO SAFETY OF HYDROGEN AND HYDROGEN SYSTEMS
|
|
ISO 11119-3:2013
|
Gas cylinders Refillable composite gas cylinders and tubes Design, construction and testing Part 3: Fully wrapped fibre reinforced composite gas cylinders and tubes up to 450L with non-load-sharing metallic or non-metallic liners
|
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